JASC 7200
Service difficulty reports · 14,730
Reports filed under 7200 · Engine (Turbine/Turboprop), newest first.
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duckdb -csv -c "SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet' WHERE jasc_code = '7200' ORDER BY difficulty_date DESC"
Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.
SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet' WHERE jasc_code = '7200' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR CA020306001Compressor · failed(CAN) THE AIRCRAFT WAS IN CRUISE FLIGHT AT FL20000. THERE WAS A LOUD BANG THAT SHUCK THE AIRCRAFT AND FLAMES APPEARED COMING OUT OF THE EXHAUST STACKS. THE ENGINE WAS SHUT DOWN AND FEATHERED. FLAMES EXTINGUISHED RIGHT AWAY IN THE STAKES. THERE WAS A SMALL AMSDR ASMF200502012Cover · missingDURING TRANSIT CHECK WAS DETECTED RIGHT ENGINE WITH COVER MISSING IN SECONDARY FLOW FAIRING. THE COVER WAS REMOVED AND THE RIGHT ENGINE WAS CHECKED BEING ON OPERATION AT LIMITS IAW P&W MM 72-00-00, INSPECTION CHECK 01 PAGE 649 ITEM 2. THE COVER WAS INSTALLEDSDR 2003F00011Engine · shutdownGTF - FLT 5031 - UNCOMMANDED NR 2 ENGINE SHUTDOWN DURING DESCENT INTO GTF AFTER POWER LEVER WAS RETARDED. UPON ARRIVAL INTO GTF, THE ENGINE, IGNITION, AND AUTO IGNITION SYSTEMS WERE INSPECTED, AND OPERATIONALLY CHECKED. THERE WERE NO DEFECTS NOTED THE AIRCRASDR CA020308009Engine · faulty(CAN) BIRD INGESTION/STRIKE ON #2 ENGINE AT TOUCHDOWN.NORMAL REVERSE USED. NO ABNORMAL ENGINE INDICATIONS IN COCKPIT. BIRD STRIKE INSPECTION CARRIED OUT NIL FAULTS FOUND.ENGINE RUN COMPLETE NIL FAULTS FOUND. THRUST REVERSER OPERATION CHECK COMPLETED NIL FAULTSSDR AUS20020118Engine · stalled(AUS) NR 1 ENGINE STALLED. VIBRATION FELT AND ENGINE PARAMETERS DIFFERENT FROM OTHER ENGINES.SDR DL76G020198Engine · vibrationON TAKEOFF ROLL, THE RIGHT ENGINE VIB INDICATED A 5.0 (LPT). TAKEOFF ABORTED AT 80 KNOTS INDICATED AIRSPEED. ALL OTHER ENGINE PARAMETERS ARE NORMAL. T/S PER FIM 71-05-00. CHIP DET CHECKED, CLEANED ACCEL CONNECTOR, LUBED FAN BLADES. PERFORMED VIBRATION SURSDR MWEA020129Engine · malfunctionedAT CRUISE ALT LEFT ENGINE MASTER CAUTION, LEFT ENGINE OIL PRESSURE LOW ANNUNCIATOR ON. LEFT ENGINE OIL PRESSURE IS ZERO. LEFT OIL TEMP IS 20 DEGREES CELSIUS AND QUANTITY IS 17-18 QUARTS. SHUT DOWN BY SELECTION. REMOVED AND REPLACED ENGINE.SDR AOQ2002F00001Engine · failedAFTER LANDING, THE FLIGHT CREW NOTED THAT THE NR 3 ENGINE OIL WARNING LIGHT ILLUMINATED. OIL PRESSURE INDICATED 25 PSI. UPON POST FLIGHT INSPECTION, CREW NOTICED OIL LEAKING FROM THE NR 3 ENGINE COWLING AND OIL FILTER BYPASS BUTTON WAS POPPED. AIRFRAME TT 9SDR AUS20020521Engine · overtemp(AUS) NR 2 ENGINE ITT EXCEEDED LIMITS.SDR AUS20020474Engine · making metal(AUS) ENGINE SURGING. INVESTIGATION FOUND METAL CONTAMINATION OF THE ENGINE.SDR CA020225004Engine · corroded(CAN) - DETERIORATION INTERNALLY- CORROSION THROUGHOUT ENGINE - WHITE POWDERSDR CA020225003Engine · deteriorated(CAN) - DETERIORATION INTERNALLY- COATING DETERIORATED ON SMALL EXIT DUCT WHICH CAUSED DAMAGE TO TURBINE BLADES.- CORROSION THROUGHOUT ENGINE (UNEXPLAINABLE) INSIDE AND OUT - WHITE POWDER.SDR ASOA02089Engine · vibrationFLT 4563 - WHILE CLIMBING OUT OF FWA, AT 21,000 FEET, THE LEFT ENGINE N2 VIBRATION SPIKED APPROXIMATELY 2.6 MILS. THE FLIGHT ATTENDANT AND PASSENGERS REPORTED A LOUD NOISE FROM THE LEFT ENGINE. THE LEFT ENGINE SHUT ITSELF DOWN. THE CAPTAIN DECLARED AN EMERGSDR CA020221017Engine · overheated(CAN) 2 MINUTES AFTER LANDING , AFTER THRUST REVERSER STOWING , THE FIRST OFFICER CALLED OUT HIGH TGT RAISING RAPIDALY AND ENGINE RUN DOWN , TEMPERATURE ROSE TO 850 DEGREES ON NR 1 ENGINE. THE TAIL PIPE FIRE DRILL WAS CARRIED OUT. MAINTENANCE CARRIED OUT ANSDR DL72L020154Engine · failedTHROUGH CLIMB NR 2 ENGINE THUMPED, EPR WENT TO 0.00, EGT ROSE. REPLACED ENGINE.SDR AWXA200200112Engine · malfunctionedONT - DIVERSION - FLT 809 - EN ROUTE FROM PHX TO SFO AND AT CRUISING ALTITUDE A NR 2 ENGINE ROLLBACK OCCURRED. THE FLIGHT CREW DECLARED AN EMERGENCY AND THE AIRCRAFT DIVERTED TO ONT. AT FL 200 THE NR 2 ENGINE WAS RESTARTED AND OPERATED NORMALLY FROM THIS TIMSDR 02FDEA00088Engine · malfunctionedAT CLIMB NR 3 ENG COUGHED AND ROLLED BACK N1 TO 35 PERCENT AND N2 50 PERCENT. EGT BEGAN TO RISE 800 DEG. SHUTDOWN ENG.SDR GLA2002F00000Bolt · backed outTAKEOFF, AC WAS CLIMBING THROUGH WHEN NR1 ENG CHIP DETECTOR/LOW PRES WARNING LIGHT ILLUMINATED. ENG WAS SHUT DOWN AND SAFE SINGLE ENG LANDING WAS MADE. INVESTIGATION REVEALED NR1 ENGINE OIL PUMP HAD RUPTURED AND FAN ASSY WOULD NOT ROTATE. ENG WAS REMOVED ANSDR G6OA064Engine · flamed outNR 3 ENGINE FLAMED OUT AT CRUISE. AFTER TROUBLESHOOTING NR 3 ENGINE, REMOVED AND REPLACED NR 3 ENGINE FUEL FILTER ELEMENT PER MM 73-11-02. REMOVED AND REPLACED NR 3 FUEL PUMP PER MM 73-12-01. REMOVED AND REPLACED MEC UNIT ON NR 3 ENGINE PER MM 73-20-01. PESDR CA020204002Bullet · separated(CAN) FLT CREW RPTED DURING CLIMB AFTER TAKEOFF THEY EXPERIENCED SERIES OF LOUD BANGS FROM NR 2 ENGINE ACCOMPANIED BY ABNORMAL HIGH EGT & LOW N 2 RPM. ALL IND.S WERE NORMAL PRIOR TO NOICE. PROBLEM OCCURRED AFTER CLIMB THRUST SET. THE CREW REDUCED NR 2 THRUST SDR 2002UALA00259Engine · malfunctionedENG TORCHING ON START DURING GROUND MAINT TEST RUN. SEVERAL COMPOSITE PANELS LT WING T/E BOTTOM OF WING JUST AFT AND TO BOTH SIDES ON NR 1 ENG HAVE HEAT DAMAGE. FUEL METERING UNIT (FMU) WAS REPLACED, COULD NOT FIND FAULT WITH UNIT. FMU PASSED AS-RECEIVED TESDR CA020308012Engine · failed(CAN) DURING FLIGHT INSPECTION OF ILS CLEARANCE ORBIT OF AIRFIELD IN SLIGHT BANK & 10-20 KTS TAILWIND NR 2 ENGINE SUDDENLY SHUTDOWN. A/C RETURNED & LANDED. ENGINEER TOOK LOOK AT ENGINE NOTHING SEEN ABNORMAL. OIL SYS CHECKED BECAUSE OF PREVIOUS EXPERIENCE WITSDR AUS20020055Engine · making metal(AUS) NR 1 ENGINE LOST POWER. OIL PRESSURE AND QUANTITY ALSO FELL. INVESTIGATION FOUND METAL IN THE SCAVENGE FILTER ON THE GEARBOX AND MASTER CHIP DETECTORS.SDR SWIA200210617Engine · vibratesNR 1 ENGINE FAN VIB IN YELLOW ARC SHORTLY AFTER TAKEOFF. ON ENGINE RUN UP, COULDN'T DUPLICATE PROBLEM. AT HIGH POWER SETTINGS, VIB NEVER GOT ABOVE .3. INSPECTED FAN BLADES VISUALLY AND INSPECTION GOOD.SDR HNAA020009Engine · making metalWHILE SETTING CRUISE POWER NR 2 ENGINE BEGAN CLANKING AND POPPING. CREW SECURED NR 2 ENGINE AND RETURNED TO DEPARTURE FIELD. MAINTENANCE FOUND METAL CONTAMINATION IN THE OIL TANK. REPLACED NR 2 ENGINE.SDR PCAA0201019Engine · damagedBWI- FLIGHT#3629. CREW REPORTED ON CLIMB AN INTERMITTANT SCREETCHING NOISE WAS HEARD WITH BOTH ENGINES AT TAKE-OFF POWER SETTINGS. NOISE WAS ACCOMPANIED BY AN INTERMITTANT VIBRATION. NOISE AND VIBRATION WENT AWAY WITH POWER REDUCTION. MAINTENANCE REPLACED LEFTSDR C2XA02CL027Engine · failedCLE FLIGHT 3052 THE CREW REPORTED THE NR 2 ENGINE SHUT DOWN IN FLIGHT UNCOMMANDED. THEY REPORTED A LOUD BANG AND HIGH ITT. THE AIRCRAFT LANDED IN CLEVELAND WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE NR 2 ENGINE.OPERATIONAL CHECKS WERE GOOD. THE AIRSDR CA020201011Engine · failed(CAN) DURING FINAL APPROACH , FLAPS 33 DEGREES , 160KNOTS ON FLIGHT TSC 372 FROM YMX TO MCO THERE WAS A HIGH VIBRATION ON NR 1 ENGINE AT 3.8 UNITS ON CHANNELS A & B. THE AIRCRAFT LANDED SAFELY AND THE ENGINE VIBRATION DRILL WAS CARRIED OUT. THE BOROSCOPE CARRSDR AUS20020054Engine · vibrates(AUS) NR 2 ENGINE VIBRATION EXCESSIVE.SDR 2002F00227Engine · failedAFTER GOOD 1.4 EPR CHECK AND WITH MAX THRUST TAKEOFF POWER SET, LOUD BANG NOTICED WITH LOSS OF EPR ON NR 2 ENGINE WHILE ROLLING TO APPROX 40 KN. ABORTED TAKEOFF AND TAXIED BACK TO RAMP, WHILE TAXIING TO RAMP PRECAUTIONARY SHUT DOWN NR 2 ENGINE. FOUND TURBINESDR HEEA077701Engine · leakingLEAKING FUEL OUT OF DRAIN WHEN ENGINE RUNNING.SDR CA020201026Engine · vibration(CAN) VIBRATION ON NR 2 ENGINE, (DURING CLIMB) INCREASING WITH ALTITUDE , ADVISORY 3.5 UNIT AT 22 000 FT AT 5.0 UNIT , FELT AIRFRAME VIBRATION. THE AIRCRAFT MADE AN AIR TURN BACK. A BLADES OFF INSPECTION WAS CARRIED OUT I.A.W. ENGINEERING ORDER 5-7231-001 SDR DJFA20020208Engine · failedDURING DESCENT, THE AIRCRAFT SHOOK FOLLOWED BY A NR 2 ENGINE CHIP DETECTOR LIGHT ILLUMINATION. ENGINE WAS SHUT DOWN AND AN UNEVENTFUL LANDING WAS MADE. UPON VISUAL EXAMINATION, THERE WERE NO EXTERNAL OIL LEAKS, THE OIL RESERVOIR WAS FOUND FULL AND THE FAN WASDR CA020201016Clamp · loose(CAN) DURING DEFECT INVESTIGATION, FOUND ON NR 1 ENGINE IN THE STRUT AREA, JUST BELOW THE REVERSE FLOW CHECK CONTROLLER, A CLAMP WITH BURNED RUBBER ON IT. PROCEEDED WITH AN AIR LEAK INVESTIGATION AND FOUND A LEAKING CLAMP. THE CLAMP WAS REPLACED.SDR DL76G020066Engine · making metalMETAL FOUND ON CHIP DETECTOR,-A- -C- AND -D- SUMP CHIP DETECTORS. ATL MTC REPLACING ENGINE. UPON FURTHER EVALUATION FROM ENGINE, SHOP NOW SUSPECT METAL IS CLEAN-UP MATERIAL. MTC FURTHER EVALUATING WITH T/O POWER PENALTY RUN.SDR RAIA00201025Engine · failed5473-STL- LEFT ENGINE CONTAM LIGHT ILLUMINATED FOLLOWED BY ENGINE IN-FLIGHT FAILURE. MAINTENANCE REMOVED AND REPLACED THE LEFT ENGINE.SDR CHQ00096Engine · failedRT ENGINE FAILED DURING T/O, AT 100 KNTS TEMP WENT TO 1000 DEG, SMOKE WENT EVERYWHERE. PULLED FIRE HANDLE AND BLEW 1 BOTTLE. REMOVED AND REPLACED RT ENGINE, FIRE BOTTLE, AND SQUIB. ALL OPS AND LEAK CHECKS GOOD.SDR AUS20020038Bearing · damaged(AUS) MASTER BALLSCREW ACTUATOR OUTPUT DRIVE LOWER BEARING BALLS MISSING AND BEARING COCKED ECCENTRICALLY. LIMITED INFORMATION PROVIDED.SDR AEO2002F00000Shaft · brokenENGINE ARRIVED FOR REPAIR OF SEIZED ROTOR CONDITION. UPON DISASSEMBLY FOUND TURBINE ROTORSHAFT SEPARATED AT BASE OF TURBINE ROTOR. THIS IS THE SECOND INSTANCE OF THIS CONDITION FOUND AT THIS REPAIR STATION. THE FAILURE WAS CONTAINED.SDR GLBA2002005Engine · fluctuatesLEFT ENGINE TORQUE FLUX. INSPECTED BLEED VALVE AND BLENDED 1ST STAGE COMPRESSOR BLADES. COULD NOT DUPLICATE. TORQUE FLUX.SDR VNAA0201014Engine · failedDURING FLIGHT, THE LEFT HAND ENGINE SHUT DOWN. THE CREW DECLARED AN EMERGENCY AND DIVERTED TO MDT. THE LEFT HAND PROPELLER DID NOT FEATHER. OUT STATION MAINTENANCE INSPECTED THE AIRCRAFT AND TROUBLESHOT THE FUEL PUMP AND HYDRO MECHANICAL UNIT, THIS DID NOT CSDR RAIA00201014Engine · fluctuates5509-EVV- ON APPROACH INTO STL, LEFT ENGINE RPM FLUX - SHUT DOWN ENGINE AS PRECAUTION. MAINTENANCE PERFORMED ENGINE OPERATIONAL CHECKS. INSTALLED HAND HELD TESTER NO FAULTS INDICATED. ENGINE OPS CHECK GOOD AT ALL POWER SETTINGS DURING ONE HOUR OF GROUND OPESDR USAABB02005Panel · looseCLT - FLT 803 - AFTER TAKEOFF, CREW NOTED AND IRRITATING, OILY ODOR IN THE COCKPIT. THE ODOR DIMINISHED WHEN THE LT PACK WAS SECURED, AND RETURNED WHEN THE PACK WAS OPERATED. THE LEFT PACK WAS SECURED FOR THE REMAINDER OF THE FLIGHT. MAINTENANCE REPLACED THSDR MEX2002317Engine · malfunctionedAIRCRAFT RETURNED TO PLATFORM DUE TO LEFT ENGINE DID NOT ACCELERATE. PARAMETERS WERE ON RIGHT ENGINE 56.5 AND ON LEFT ENGINE 51.0 ENGINE 51.0. ENGINES WERE ADJUSTED ON IDLE, TESTS OK. DURING OVERNIGHT, SERVICE WAS PERFORMED A TRIM TO BOTH ENGINES IAW MM, TESDR SIMA200201001Engine · malfunctionedDFW - FLT 3826 - ON DESCENT, LEFT ENGINE TQ WENT TO MAX, GOT OVERTEMP LIGHT. CREW SHUT LEFT ENGINE DOWN. (M)SDR ARWA20020110Engine · malfunctionedNR 2 ENGINE STARTS AFTER 2 MINUTES ENGINE ROLL BACK TO ZERO AND SHUT DOWN.SDR CA020110010Engine · failed(CAN) NR 1 ENGINE LOST OIL PRESSURE AT 31,000 FT. PERFORMED IN-FLT SHUT-DOWN. DECLARED EMERGENCY AND LANDED. INSPECTED ENGINE FOR LEAKS, SERVICING AND GROUND RUNS, NOTHING UNUSUAL FOUND. FERRIED TO CVG FOR FUTHER INVEST. NO ABNORMALITIES NOTED DURING SDR CA020110012Carbon Seal · leaking(CAN) AS CREW WAS CLIMBING THROUGH 27,000 FT, RECEIVED RT ENGINE OIL PRESSURE MESSAGE. CREW SHUT DOWN RT ENGINE AND CONTINUED ON TO ATL. ONCE IN ATL, MAINTENANCE FOUND THE ENGINE 6 QUARTS LOW OF OIL. EVENTUALLY, OIL LEAKAGE WAS FOUND IN THE C-SUMP AREA. THESDR WVE2002F00000Solenoid · failedLEFT ENGINE FAILED IN FLIGHT, ATTEMPTED RESTART, ENGINE TEMPERATURE HIGH AND VIBRATION CAUSED ABORT ATTEMPT. PROBABLE CAUSE: BOV SOLENOID AND/OR HMU FAILED. THE ENGINE WAS BORESCOPED WITH NO SIGNIFICANT FINDINGS. THE IGNITERS(2EA) PN31B5168-01 SERIAL NUMBSDR 00009Engine · flamed outDURING CLIMB THROUGH FLT LEVEL 43.8 LT ENGINE FLAMED-OUT, AT FL250 AIRSTART PERFORMED AND CONTINUED FLT AT 370. PILOT PERFORMED VISUAL INSPECTION OF ENGINE AND FUEL SAMPLE. ENGINE INSPECTED AT YIP BY MAINTENANCE WITH NO DEFECTS NOTED.
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